Purpose
This Volume establishes requirements for the management of Defence Aviation Safety by commanders and managers.
Structure
The Defence Aviation Safety Regulation (DASR) is comprised of:
General Requirements (GR), which are set out below in two subparts:
Subpart A Scope and applicability defines the scope of the DASR and the applicability of the DASR parts.
Subpart B Common requirements and provisions establishes requirements and provisions that are each applicable to a significant proportion of regulated entities.
the DASR parts, which are set out in Annex A.
DASR clauses and sub-clauses may have associated supporting information in the form of:
Acceptable Means of Compliance (AMC). AMC is information published by DASA to identify a means of meeting one or more requirements of the DASR. Regulated entities are not required to comply with AMC and may instead propose an Alternative Means of Compliance to DASA. Any such proposal will be subject to separate assessment by DASA to determine whether the approach is compliant with the DASR.
Guidance Material (GM). GM provides additional explanation to assist the application of the requirement and/or explain the AMC.
Context
This Volume implements applicable requirements set out in DASP Manual Volume 1 Requirements for the DASP.
DASP Manual Volume 3 DASP Guidance provides further information to support understanding of, and compliance with, the DASR.
Definitions
The following definitions apply within this Volume and its annex:
Continuing Airworthiness. All of the processes ensuring that, at any time in its operating life, an aircraft complies with the airworthiness requirements in force and is in a condition for safe operation.
Defence Personnel. All Australian Public Service employees in the Department of Defence, Defence locally engaged employees, Defence civilians, Defence members and the equivalents from other Defence organisations on exchange to Defence.
Defence Registered Aircraft. An aircraft listed on the Defence aircraft register maintained by DASA.
State Aircraft. Aircraft of any part of the Defence Force (including any aircraft that is commanded by a member of that Force in the course of duties as such a member); and aircraft used in the military, customs or police services of a foreign country. This includes Uncrewed Aircraft Systems (UAS).
Further definitions are available in the DASP Glossary.
State Aircraft operated by Defence must be:
Defence Registered Aircraft; or
managed in accordance with DASR NDR Non-Defence Registered aircraft.
Paragraph (a) is not applicable to Uncrewed Aircraft Systems except as required by DASR UAS Uncrewed Aircraft Systems.
The design, production and certification of Defence Registered Aircraft must be managed in accordance with DASR 21 Aircraft Design, Production and Certification.
The Continuing Airworthiness of Defence Registered Aircraft, and components thereof, must be managed in accordance with:
DASR M Continuing Airworthiness Management
DASR 145 Requirements for Maintenance Organisations
DASR 66 Military Aircraft Maintenance Licencing
DASR 147 Aircraft Maintenance Training Organisations.
Personnel and organisations involved in Defence aviation operations must comply with:
DASR MED Medical
DASR AVFM Aviation Fatigue Management
DASR NTS Non-Technical Skills.
Paragraph (a) is not applicable to Uncrewed Aircraft Systems except as required by DASR UAS Uncrewed Aircraft Systems.
The operation of State Aircraft by Defence must be in accordance with:
DASR AO.Gen Air Operations – General
DASR ARO Authority Requirements for Air Operations
DASR ORO Organisation Requirements for Air Operations
DASR NDR Non-Defence Registered aircraft
DASR SPA Specific Purpose Approval
DASR SPO Special Purpose Operations
DASR UAS Uncrewed Aircraft Systems
DASR FT Flight Tests
Defence Registered Aircraft must have a valid type-certificate11 to conduct operations. The type-certificate must be issued in accordance with DASR 21 Subpart B Military Type-Certificates and Military Restricted Type-Certificates.
Defence Registered Aircraft must have a valid certificate of airworthiness22 to conduct operations. The certificate must be issued in accordance with DASR 21 Subpart H Military Certificates of Airworthiness and Military Restricted Certificates of Airworthiness.
Flight Simulation Training Devices and their use must be managed in accordance with DASR FSTD Flight Simulation Training Devices.
Defence Aerodromes, including shipborne heliports, must be operated, managed and certified in accordance with DASR 139 Aerodromes.
The provision of Air Traffic Management services and Air Navigation Services by Defence, including equipment, systems, and organisations must be in accordance with:
DASR ANSP Air Navigation Service Providers; and
the regulations identified by GR.20 Operations personnel, as applicable.
The provision of Air Battle Management operations conducted by Defence, including equipment, systems and organisations, must be in accordance with:
DASR ABM Air Battle Management
the regulations identified in GR.20 Operations personnel, as applicable
DASR AO.GEN.05 Management of OIP.
Where required by other DASR, regulated entities must report aviation safety occurrences to DASA in a form and manner acceptable to DASA.AMCAMC
AMC GR.40 identifies which aviation safety occurrences should be reported to the Authority, and details the timescale for submission of such reports. It also describes the objective of the overall occurrence reporting system including internal and external functions.
This AMC applies to occurrence reporting by persons / organisations regulated by the Defence Aviation Safety Regulation (DASR). In most cases the obligation to report is on the holders of a certificate or approval, which are primarily organisations, but in some cases may be an individual. In addition some reporting requirements are directed to persons. However, in order not to complicate the text, only the term ‘organisation’ is used throughout this AMC.
NOTE: This AMC does not apply to dangerous goods or explosive ordnance reporting.
Objective of Occurrence Reporting
The occurrence reporting system is an essential part of the overall monitoring function. The objective of the occurrence reporting, collection, investigation and analysis systems described in operating and airworthiness regulation, is to use the reported information to contribute to accident prevention, the improvement of aviation safety, and not to attribute blame, or take other enforcement actions.
The detailed objectives of the occurrence reporting systems are:
To enable an assessment of the safety implications of each occurrence to be made, including previous similar occurrences, so that any necessary action can be initiated. This includes determining what and why it had occurred and what might prevent a similar occurrence in the future.
To ensure that knowledge of occurrences is disseminated so that others may learn from them.
The occurrence reporting system is complementary to the normal day to day procedures and 'control' systems and is not intended to duplicate or supersede any of them. The occurrence reporting process is to identify those occasions where controls have failed.
Occurrences should remain in the databases when judged non-reportable by the person submitting the report as the significance of such reports may only become obvious at a later date.
Requirements:
Occurrences are defined as an incident, malfunction, defect, technical defect or exceedance of limitations that endangers or could endanger the safe operation of aircraft and must be reported to the Authority.
Reporting does not remove the reporter’s or organisation’s responsibility to commence corrective actions to prevent similar occurrences in the future. Known and planned preventive actions should be included within the report.
NOTE: Section I to IV of this AMC identifies what should be reported by an organisation or individual to the Authority.
Where applicable and relevant, other (domestic and international) civil and military aviation safety authorities should be advised of the occurrences.
General. There are different reporting requirements for operators (and/or commanders), maintenance organisations, design organisations and production organisations. The criteria for all these different reporting lines are not the same. For example, the Authority will not receive the same kind of reports from a design organisation as from an operator or an Air Navigation Service Provider. This is a reflection of the different perspectives of the organisations based on their activities.
Many of the occurrences which are considered ‘reportable occurrences’ for crewed aircraft would not endanger safe operation of a UAS due to the absence of people on board. As such, reportable occurrences for UAS are found in the UAS implementing regulations.
List of reportable occurrences. Section I to IV is a list of reportable occurrences. Not all examples are applicable to each reporting organisation.
Section I - Aircraft Flight OperationsSection I - Aircraft Flight Operations
Under DASR Phase 1, reporting of Aircraft Flight Operations based occurrences using the Hazard Reporting and Tracking framework articulated within the Defence Aviation Safety Manual, and supporting procedures meets the intent of this SECTION.
A listing of specific Authority reportable Aircraft Flight Operations based occurrences will be consulted / promulgated in 2018.
Section II - Aircraft TechnicalSection II - Aircraft Technical
This section is structured in such a way that the pertinent occurrences are linked with categories of activities during which they are normally observed, according to experience, in order to facilitate the reporting of those occurrences. However, this presentation must not be understood as meaning that occurrences must not be reported in case they take place outside the category of activities to which they are linked in the list.
Structural
For Structural Integrity (SI), an unsafe condition is not always obvious. Engineering judgement is required to decide whether defects or damage is serious enough to be reported, if in doubt advice should be sort. The following examples can be taken into consideration:
Defect or damage that may affect structural strength or life, to critical structure exceeding admissible damage or where no pre-approved repair exists from previous investigation activity. Critical structure is that which contributes significantly to carrying flight, ground, and pressurisation loads, and whose failure could result in a catastrophic failure of the aircraft.
Damage to or defect exceeding allowed tolerances of structural element which failure could reduce the structural stiffness to such an extent that the required flutter, divergence or control reversal margins are no longer achieved.
Damage to or defect of a structural element, which could result in the liberation of items of mass that may injure occupants of the aircraft.
Damage to or defect of a structural element, which could jeopardise proper operation of systems. See SYSTEMS (including software) below.
Loss of any part of the aircraft structure in flight.
Systems (including software)
The following generic criteria applicable to all systems are proposed: Loss, significant malfunction or defect of any system, subsystem or set of equipment that could endanger flight safety when standard operating procedures, drills etc, could not be satisfactorily accomplished.
Inability of the crew to control the system, for example:
uncommanded actions;
incorrect and or incomplete response, including limitation of movement or stiffness;
runaway;
mechanical disconnection or failure.
Failure or malfunction of the exclusive function(s) of the system (one system could integrate several functions).
Interference within or between systems.
Failure or malfunction of the protection device or emergency system associated with the system.
Loss of redundancy of the system.
Any occurrence resulting from unforeseen behaviour of a system.
Leakage of hydraulic fluids, fuel, oil or other fluids which resulted in a fire hazard or possible hazardous contamination of aircraft structure, systems or equipment, or risk to occupants.
Malfunction or defect of any indication system when this results in the possibility of misleading indications to the crew.
Any failure, malfunction or defect if it occurs at a critical phase of flight and relevant to the operation of that system.
Asymmetry of flight controls; eg flaps, slats, spoilers.
Enclosure 1 to SECTION II, gives a list of examples of reportable occurrences resulting from the application of these generic criteria to specific systems.
Propulsion Systems (including engines, propellers, rotor systems and transmissions) and Auxiliary Power Units (APU)
Engines. The following criteria applicable to engines are proposed:
Overspeed or inability to control the speed of any high speed rotating component, for example: auxiliary power unit, air starter, air cycle machine, air turbine motor, propeller or rotor.
Failure or malfunction of any part of an engine or powerplant resulting in any one or more of the following:
non containment of components/debris;
uncontrolled internal or external fire, or hot gas breakout;
thrust in a different direction from that demanded by the pilot;
thrust reversing system failing to operate or operating inadvertently;
inability to control power, thrust or rpm;
failure of the engine mount structure;
partial or complete loss of a major part of the powerplant;
Dense visible fumes or concentrations of toxic products sufficient to incapacitate crew or passengers;
inability, by use of normal procedures, to shutdown an engine;
inability to restart a serviceable engine.
A flameout, uncommanded thrust/power loss or malfunction:
for a single engine aircraft; or
where it is considered excessive for the application, or
where this could affect more than one engine in a multi-engine aircraft, particularly in the case of a twin engine aircraft; or
for a multi engine aircraft where the same, or similar, engine type is used in an application where the event would be considered hazardous or critical.
Any defect in a propulsion system critical part causing retirement before completion of its full life.
Defects of common origin which could cause an in flight shut down rate so high that there is the possibility of more than one engine being shut down on the same flight.
An engine limiter or control device failing to operate when required or operating inadvertently.
Exceedance of engine parameters.
Volcanic ash encounter.
Propellers and transmission.
Failure or malfunction of any part of a propeller or powerplant resulting in any one or more of the following:
an overspeed of the propeller;
the development of excessive drag;
a thrust in the opposite direction to that commanded by the pilot;
a release of the propeller or any major portion of the propeller;
a failure that results in excessive unbalance;
the unintended movement of the propeller blades below the established minimum in-flight low-pitch position;
an inability to feather the propeller;
an inability to command a change in propeller pitch;
an uncommanded change in pitch;
an uncontrollable torque or speed fluctuation;
The release of low energy parts.
Rotors and transmission:
Damage or defect of main rotor gearbox or attachment which could lead to in flight separation of the rotor assembly, and /or malfunction/loss of rotor control.
Damage or defect to tail rotor, transmission and equivalent systems.
Auxiliary Power Units:
Shut down or failure when the APU is required to be available by operational requirements, eg Defence Long Range Operations (DLRO) / Extended Twin-engined Operations (ETOPS) / Extended Range Operations (EROPS), Minimum Equipment List (MEL).
Inability to shut down the APU.
Overspeed.
Inability to start the APU when needed for operational reasons.
The following give examples of reportable occurrences resulting from application of the generic criteria to specific systems listed under SYSTEMS (including software), in SECTION II.
Air conditioning / ventilation
complete loss of avionics cooling
depressurisation
Autoflight system
failure of the autoflight system to achieve the intended operation while engaged
significant reported crew difficulty to control the aircraft linked to autoflight system functioning
failure of any autoflight system disconnect device
uncommanded autoflight mode change
Bleed air system
hot bleed air leak resulting in a fire warning or structural damage
loss of bleed air systems
failure of bleed air leak detection system
Cockpit / cabin / cargo
pilot seat control loss during flight
failure of any emergency system or equipment, including emergency evacuation
signalling system, all exit doors, emergency lighting, etc
loss of retention capability of cargo loading system
Communications
total loss of communication in flight
Electrical system
loss of one electrical system distribution system (AC or DC)
total loss or loss of more than one electrical generation system
failure of back-up (emergency) electrical generating system
serious damage to electrical wiring and interconnection system (EWIS)
Explosive ordnance
inadvertent release of stores due to mechanical or system failure
hung store
stores management system failure
Fire protection system
fire warnings, except those immediately confirmed as false
undetected failure or defect of fire/smoke detection/protection system, which could lead to loss or reduced fire detection/protection
absence of warning in case of actual fire or smoke
Flight controls
asymmetry of flaps, slats spoilers, etc
limitation of movement, stiffness or poor or delayed response in the operation primary
Flight control surface runaway
mechanical flight control disconnection or failure
significant interference with normal control of the aircraft or degradation of flying qualities
Fuel system
fuel quantity indicating system malfunction resulting in total loss or erroneous indicated fuel quantity on board
leakage of fuel which resulted in major loss, fire hazard, significant contamination
malfunction or defects of the fuel jettisoning system which resulted in advertent loss of significant quantity, fire hazard, hazardous contamination of aircraft equipment or inability to jettison fuel
fuel system malfunctions or defects which had a significant effect on fuel supply and/or distribution
Hydraulics
loss of one hydraulic system (extended twin-engined operations (ETOPS) only)
failure of the isolation system to operate
loss of more than one hydraulic circuit
failure of the back-up hydraulic system
inadvertent Ram Air Turbine extension
Ice detection / protection system
undetected loss or reduced performance of anti ice/de-ice system
loss of more than one of the probe heating systems
inability to obtain symmetrical wing de-icing
abnormal ice accumulation leading to significant effects on performance or handling qualities
crew vision significantly affected
Indicating / warning / recording systems
malfunction or defect of any indicating system when the possibility of significant misleading indications to the crew could result in an inappropriate crew action on an essential system
for glass cockpits: loss or malfunction of more than one display unit or computer involved in the display/warning function
Landing gear system / brakes / tyres
brake fire
significant loss of braking action
unsymmetrical braking leading to significant path deviation
failure of the landing gear free fall extension system (including during scheduled tests)
unwanted landing gear or landing gear doors extension/retraction
multiple tyre bursts
Navigation systems (including precision approaches system) and air data systems
total loss or multiple navigation equipment failures
total failure or multiple air data system equipment failures
significant misleading indication
significant navigation errors attributed to incorrect data or a database coding error
unexpected deviations in lateral or vertical path not caused by pilot input
problems with ground navigational facilities leading to significant navigation errors not associated with transitions from inertial navigation mode to radio mode
Oxygen
for pressurised aircraft: loss of oxygen supply in cockpit
loss of oxygen supply to a significant number of passengers, (more than 10%),including when found during maintenance or training or test purposes
Section III - Aircraft Maintenance and RepairSection III - Aircraft Maintenance and Repair
This section is structured in such a way that the pertinent occurrences are linked with categories of activities during which they are normally observed, according to experience, in order to facilitate the reporting of those occurrences. However, this presentation must not be understood as meaning that occurrences must not be reported in case they take place outside the category of activities to which they are linked in the list.
Maintenance and Maintenance Related
Incorrect assembly of parts or components of the aircraft found during an inspection or test procedure not intended for that specific purpose.
Hot bleed air leak resulting in structural damage.
Identified burning, melting, smoke, arcing, overheating or fire occurrences.
Any defect in a critical structure or propulsion system critical part causing retirement before completion of its full life.
Any damage or deterioration, ie fractures, cracks, corrosion, delamination, disbonding, (size is by no means a reliable indication of significance) resulting from any cause (such as flutter, loss of stiffness or structural failure) to:
Critical structure (as defined by the certified type design) where such damage or deterioration exceeds allowable limits specified in the Repair Manual and requires a repair or complete or partial replacement of the structure;
secondary structure which consequently has or may have endangered the aircraft; or
the engine, propeller or rotorcraft rotor system.
Exceedance of critical structure or propulsion system critical part airworthiness limitations or maintenance requirements.
Any failure, malfunction or defect of any system or equipment, or damage or deterioration found as a result of compliance with an Airworthiness Directive or other mandatory instruction issued by a Regulatory Authority, when:
it is detected for the first time by the reporting organisation implementing compliance;
on any subsequent compliance where it exceeds the permissible limits quoted in the instruction and/or published repair/rectification procedures are not available.
Failure of any emergency system or equipment, including all exit doors and lighting, to perform satisfactorily, including when being used for maintenance or test purposes.
Non compliance or significant errors in compliance with required maintenance procedures.
Wrong assessment of a serious defect, or serious non-compliance with the Minimum Equipment List (MEL) and Technical logbook procedures.
Incorrect control or application of aircraft maintenance limitations or scheduled maintenance.
Releasing an aircraft to service from maintenance in case of any non-compliance which endangers the flight safety.
Serious damage caused to an aircraft during maintenance activities due to incorrect maintenance or use of inappropriate or unserviceable ground support equipment that requires additional maintenance actions.
Any occurrence where the human performance, including fatigue of personnel, has directly contributed to or could have contributed to an accident or a serious incident.
Products, parts, appliances and materials of unknown or suspect origin.
Misleading, incorrect or insufficient maintenance data or procedures that could lead to maintenance errors, which could endanger flight safety.
Failure, malfunction or defect of ground equipment used for test or checking of aircraft systems and equipment when the required routine inspection and test procedures did not clearly identify the problem when this results in a hazardous situation, which could endanger flight safety.
Significant malfunction, reliability issue, or recurrent recording quality issue affecting a flight recorder system (such as a flight data recorder system, a data link recording system or a cockpit voice recorder system) or lack of information needed to ensure the serviceability of a flight recorder system.
Under DASR Phase 1, reporting of Air Navigation Services (ANS), Aerodrome (ADR) and Ground based occurrences using the Hazard Reporting and Tracking framework articulated within the Defence Aviation Safety Manual, and supporting procedures meets the intent of this Section.
A listing of specific Authority reportable ANS, ADR and Ground-based occurrences will be consulted / promulgated in 2018.
Reportable occurrences are those where the safety of operation was or could have been endangered or which could have led to an unsafe condition. If in the view of the reporter an occurrence did not hazard the safety of the operation but if repeated in different but likely circumstances would create a hazard, then a report should be made.
Immediate Notification of Accidents and Serious Incidents
Accidents and Serious Incidents are serious occurrences (deaths, serious injury and serious damage to aircraft and property or had a high potential/likelihood to do so due to the lack or remaining controls) require additional and immediate notification to the aviation safety investigation Authority. This immediate reporting requirement extends to any occurrence where there is an exposure to a serious risk of death, injury or damage.
The need to report an occurrence in accordance with this AMC does not immediately constitute the need to conduct Accident or Serious Incident investigation.
List of immediately notifiable occurrences. Section V is a list of accidents and serious incidents that require immediate notification to the aviation safety investigation Authority. It is possible for occurrences listed under Reportable Occurrences above, (SECTIONs I to IV), to be further categorised as serious incidents and would therefore subject to immediate notification requirements. In these instances professional judgement is required. Section V - Immediate Notification of Accidents and Serious IncidentsSection V - Immediate Notification of Accidents and Serious Incidents
It is possible for occurrences not listed here to be further categorised as serious incidents and therefore subject to immediate notification requirements. In this instance professional judgement is required. Categorisation of these occurrences into accidents or serious incidents, is often circumstance dependent so it is most important to note that the categorisation of any occurrence should only be finalised after a thorough examination of all the circumstances of that occurrence.
The immediate notification of Accidents and Serious Incidents should occur as soon as is reasonably practicable.
Accident:
Death of any person
Loss of an aircraft, ie unrepairable, missing or inaccessible for recovery.
Serious Incident.
The list is not exhaustive and only serves as guidance to the definition of serious incident.
Near collisions requiring an avoidance manoeuvre to avoid a collision or an unsafe situation or when an avoidance action would have been appropriate.
Controlled flight into terrain only marginally avoided.
Aborted take-offs on a closed or engaged runway, on a taxiway1 or unassigned runway.
Take-offs from a closed or engaged runway, from a taxiway2 or unassigned runway.
Landings or attempted landings on a closed or engaged runway, on a taxiway3 or unassigned runway.
Gross failures to achieve predicted performance during take-off or initial climb.
Fires and smoke in the passenger compartment, in cargo compartments or engine fires, even though such fires were extinguished by the use of extinguishing agents.
Events requiring the emergency use of oxygen by the flight crew.
Aircraft structural failures or engine disintegrations, including uncontained turbine engine failures, not classified as an accident.
Multiple malfunctions of one or more aircraft systems seriously affecting the operation of the aircraft.
Flight crew incapacitation in flight.
Fuel quantity requiring the declaration of an emergency by the pilot.
Runway incursions.
Take-off or landing incidents. Incidents such as under-shooting, overrunning or running off the side of runways.
System failures, weather phenomena, operations outside the approved flight envelope or other occurrences which could have caused difficulties controlling the aircraft.
The reporting time starts from when the occurrence took place or from the time when the reporter determined that there was, or could have been, a potentially hazardous or unsafe condition. The immediate notification of Accidents and Serious Incidents should occur as soon as reasonably practicable.
The reporting period for all other occurrences that have not required immediate notification is 72 hours. Within the overall limit of 72 hours for the submission of a report, the degree of urgency should be determined by the level of hazard judged to have resulted from the occurrence. Subsequent reporting from organisations made aware of an occurrence is to be within 72 hours of initial notification.
Notwithstanding other required reporting means as promulgated by other legislation, regulation or policy, reports may be transmitted in any form considered acceptable to the Authority. The amount of information in the report should be commensurate with the severity of the occurrence. Each report should at least contain the following elements, as applicable to each organisation:
Organisation details
Information necessary to identify the affected:
aircraft and / or component affected, including software version (if applicable),
ANS system,
Aerodrome.
Date and time if relevant
Summary description of the occurrence
Any other specific/ relevant information
For any occurrence involving a system or component, which is monitored or protected by a warning and/or protection system, for example: fire detection/extinguishing or separation alert, the occurrence report should always state whether such system(s) functioned properly.
Reporting Between Organisations
Requirements exist that address the reporting of data relating to unsafe or unairworthy conditions. These reporting lines are:
Production Organisation to the organisation responsible for the design;
Maintenance organisation to the organisation responsible for the design;
Maintenance organisation to operator;
Operator to organisation responsible for the design;
Production organisation to production organisation;
Design organisation to production organisation.
The ‘Organisation responsible for the design’ is a general term, which can be any one or a combination of the following organisations:
Holder of a Military Type-certificate (MTC) of an Aircraft, Engine or Propeller.
Holder of a Military Supplemental Type-certificate (MSTC) on an Aircraft, Engine or Propeller.
Holder of an Approved Design.
NOTE: In the ADF context this usually means the Systems Program Office (SPO) with embedded Military Type-certificate holder, Total Logistics Support Contractor, or both. If it can be determined that the occurrence has an impact on or is related to other aircraft types then the holders of such approval/authorisation should be informed. Figure 1 presents a simplified scheme of reporting lines for Initial and Continuing Airworthiness organisations.
Figure 1 - Reporting Lines
Regulated entities must cooperate with DASA with a view to assuring compliance with the DASR.
For the purposes of the implementation of paragraph (a), regulated entities must conduct investigations, including ramp inspections, and must take any measure to prevent the continuation of a non-compliance.
In order to facilitate the taking of appropriate enforcement action by competent authorities, regulated entities shall exchange information on identified infringements with DASA.
An interpretation of Finding Levels in the context of DASR 147 are as follows:
DASR 147 Level 1 Finding – A non-compliance that ‘lowers the safety standard and seriously hazards flight safety’ in a DASR 147 environment would result from a critical failure of a training product that degrades training outcomes impacting airworthiness. Examples might include a failure to follow established training procedures that have a direct impact to training outcomes, significant deviation from approved training product, significant unapproved changes to the training organisation, or awarding training outcomes that have not been fully achieved.
DASR 147 Level 2 Finding – A non-compliance that ‘lowers the safety standard and possibly hazards flight safety’ in a DASR 147 environment would result from a major failure of a training product or a major failure to comply with training governance requirements that has the possibility to degrade training outcomes impacting airworthiness. Examples might include a deviation in training processes that impacts training outcomes or a major deviation from approved training product.
DASR 147 Level 3 Finding – A non-compliance, or potential problem, that ‘could lower the safety standard and possibly hazard flight safety’ in a DASR 147 environment would result from a minor failure of a training product or minor failure to comply with training governance requirements. Examples might include minor errors in documentation or minor procedural deviations that if left untreated could manifest into a lowering of safety standards, or a minor failure to achieve training governance requirements.
Root-cause Analysis
It is important that the analysis does not primarily focus on establishing who or what caused the non-compliance but why it was caused. Establishing the root causes of a non-compliance often requires an overarching view of the events and circumstances that led to it, to identify all possible systemic and contributing factors (regulatory, human factors, organisational, managerial, cultural, technical, etc) in addition to the direct factors. A narrow focus on single events or failures, or the use of a simple method such as fault tree, to identify the chain of events that led to the non-compliance may not properly reflect the complexity of the issue. This may then give rise to the risk that important factors that are required to be addressed in order to prevent recurrence will be ignored.
Such inappropriate or partial root-cause analysis often leads to defining ‘quick fixes’ addressing the symptoms of the non-compliance only. A peer review of the results of the root-cause analysis may increase its reliability and objectivity.
A system description of the organisation considering organisational structures, processes and their interfaces, procedures, staff, equipment, facilities and the environment in which the organisation operates will support both effective root-cause (reactive) and hazard (proactive) analysis.
Corrective Actions
Corrective action is the action to eliminate or mitigate the root causes and prevent recurrence of an existing detected non-compliance, or other undesirable condition or situation. Proper determination of the root cause is crucial for defining effective corrective actions to prevent recurrence.
Corrective Action Plan
The corrective action plan links individual root causes and corrective actions defining the strategy to prevent non-compliance recurrence. It documents the expected objective quality evidence required to validate the effectiveness of the corrective action and the timeline for implementation (inclusive of collective evidence to validate effectiveness) of each corrective action.
(Reserved)
Where an equivalent level of protection to that attained by the application of the DASR can be achieved by other means, DASA may approve exception from those DASR.
DASA may allow a credible and defensible level of military aviation safety performance where an equivalent level of protection to that provided by the application of the DASR cannot be demonstrated, but can be supported by the application of sound risk management principles.GMGM
This regulation recognises that Defence is a military force that sometimes needs to operate at levels of risk greater than would be acceptable to national civil aviation authorities. Such increased risks may result from:
incomplete type certification activities without sufficient controls to achieve the safety requirements, due, for example, to:
production inconsistencies or flaws
uncertainty about original certification basis requirements for long-serving legacy aircraft and aerodromes; and
an inability to obtain, for acquired aircraft, adequate disclosure of the original certification basis requirements on which Defence will base its military type certification.
operational imperatives necessitating unairworthy aircraft to be operated; that is the certificate of airworthiness is invalid.
operating imperatives necessitating operations outside the scope of the MAOC (such as for specific missions and crew compositions, specific flying orders not being able to be met).
enduring operational imperatives such as an inability to achieve desired capability outcomes whilst compliant with contemporary crash protection requirements.
The flexibility provided by this regulation allows Defence, inter alia, to operate outside a type certification basis, to operate outside the scope of the MAOC, to operate with open 'design/type certification' issue papers, as well as continued operations with known unserviceabilities, unrepaired damage or deferred maintenance, eg where the certificate of airworthiness is invalid.
This flexibility provision does not exempt Defence from a duty under the Australian Work Health and Safety (WHS) Act. Consequently, where operations under the flexibility provision are contemplated, the risks to health and safety of persons must be eliminated so far as is reasonably practicable and if this is not possible then reduced so far as is reasonably practicable in the circumstance.
DASA must acknowledge that regulated organisations may deviate from the substantive requirements laid down in this Regulation in the event of compelling operational imperatives or emergencies.GMGM
This regulation continues the long-standing flexibility arrangement whereby operational commanders may deviate from aviation safety requirements in an emergency or compelling circumstance. Such deviations should only be made where there is insufficient time either to seek:
permit to fly as described in DASR Subpart P, or
prior Authority approval for an exception or a reduced level of protection as provided for at GR.80 (b) and GR.80 (c) respectively.
DASR 21 Aircraft Design, Production and Certification
DASR 66 Military Aircraft Maintenance Licencing
DASR 139 Aerodromes
DASR 145 Requirements for Maintenance Organisations
DASR 147 Aircraft Maintenance Training Organisations.
DASR ABM Air Battle Management
DASR ANSP Air Navigation Service Providers
DASR AO.Gen Air Operations General
DASR ARO Authority Requirements for Air Operations
DASR AVFM Aviation Fatigue Management
DASR FSTD Flight Simulation Training Devices
DASR FT Flight Tests
DASR M Continuing Airworthiness Management
DASR MED Medical
DASR NDR Non-Defence Registered aircraft
DASR NTS Non-Technical Skills
DASR ORO Organisation Requirements for Air Operations
DASR SMS Aviation Safety Management Systems
DASR SPA Specific Purpose Approval